The effect of area aspect ratio on the yawing moments of rudders at large angles of pitch on three fuselages (1933)
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int on the fuselage near the the fixed surface, which had been aligned with the tail to a balance of the pendulum type. A counter- axis of the model. The axis of the model was set at weight was used when necessary to maintain tension the desired angle of pitch and at 0° yaw with respect in the… … Fmtoe 4.—Cabin fuselage obtained on airfoils in the normal and inverted posi- tions and from yawmeter readings. ^Socket plate Wind tunnel and balance arrangement.—The meas- -End plate ? Tivot urements were made in the 10-foot wind tunnel of BtaUBE 6.—Method of hinging rudders the Bureau of…
NASA Technical Reports Server (NTRS)
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